SAE AMS2301K
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
STEEL CLEANLINESS, AIRCRAFT QUALITY MAGNETIC PARTICLE INSPECTION PROCEDURE
Available format(s)
Hardcopy , PDF
Superseded date
22-05-2020
Superseded by
Language(s)
English
Published date
01-01-2015
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
Specifies steel cleanliness requirements in inch/pound units for aircraft-quality ferro-magnetic steels, other than hardenable corrosion resistant steels, by magnetic particle inspection methods.
| Committee |
AMS-E
|
| DevelopmentNote |
Supersedes SAE MAM 2301. (07/2007)
|
| DocumentType |
Standard
|
| Pages |
14
|
| PublisherName |
SAE International
|
| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| MIL-S-6758 Revision B:1993 | STEEL, CHROME-MOLYBDENUM (4130) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) |
| SAE AMS6299F | STEEL BARS, FORGINGS, AND TUBING, CARBURIZING, 0.50CR - 1.8NI - 0.25MO (0.17 - 0.23C) (SAE 4320H) |
| SAE AMS6263M | STEEL BARS, FORGINGS, AND TUBING, 1.2CR - 3.2NI - 0.12MO (0.11 - 0.17C) (9315) |
| SAE AMS6350N | STEEL SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130) |
| SAE AMS6327L | STEEL BARS AND FORGINGS, 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740), HEAT TREATED, 125 KSI (862 MPA) TENSILE STRENGTH (COMPOSITION SIMILAR TO UNS G87400) |
| SAE AMS6351K | STEEL, SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), SPHEROIDIZED |
| MIL S 81081 : A | STEEL; SHEET, CHROMIUM NICKEL MOLYBDENUM VANADIUM (FOR TORPEDO MARK 46 MOD O) |
| SAE AMS6328N | STEEL, BARS, FORGINGS, AND TUBING, 0.50CR - 0.55NI - 0.25MO (0.48 TO 0.53C) (SAE 8750) |
| SAE AMS6434H | STEEL, SHEET, STRIP, AND PLATE, 0.78CR - 1.8NI - 0.35MO - 0.20V (0.33 - 0.38C) (4335 MOD) |
| SAE AMS6433G | STEEL, SHEET, STRIP, AND PLATE 0.75MN - 0.78CR - 1.8NI - 0.35MO - 0.20V (0.33 - 0.38C) (4335 MOD) |
| SAE AMS6361F | STEEL TUBING, SEAMLESS, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130) 125 KSI (862 MPA) TENSILE STRENGTH |
| SAE AMS6282J | STEEL TUBING, MECHANICAL, 0.50CR - 0.55NI - 0.25MO (0.33 - 0.38C) (SAE 8735) |
| SAE AMS 6492 : 2013 | STEEL BARS, FORGINGS, AND TUBING, 1.0CR - 3.25NI - 0.40MO (0.17 - 0.22C) AIRCRAFT QUALITY |
| SAE AMS6302K | LOW-ALLOY STEEL, HEAT-RESISTANT, BARS, FORGINGS, AND TUBING, 0.65SI - 1.25CR - 0.50MO - 0.25V (0.28 - 0.33C) |
| SAE AMS6303J | STEEL BARS AND FORGINGS, LOW ALLOY, HEAT-RESISTANT, 0.65SI - 1.25CR - 0.50MO - 0.85V (0.25 - 0.30C) |
| SAE AMS6360M | STEEL TUBING, SEAMLESS, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), NORMALIZED OR STRESS RELIEVED |
| MIL-HDBK-1587 Base Document:1996 | MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM |
| SAE AMS6396F | STEEL SHEET, STRIP, AND PLATE, 0.80CR - 1.8NI - 0.25MO (0.49 - 0.55C) ANNEALED |
| SAE AMS6352K | STEEL SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.33 - 0.38C) (SAE 4135) |
| MIL-STD-1587 Revision D:2017 | MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
| BS 5S 100:1993 | Procedure for inspection, testing and acceptance of wrought steels (other than plate, sheet, strip and tube) |
| SAE AMS6370P | STEEL, BARS, FORGINGS, AND RINGS, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130) |
| SAE AMS6322P | STEEL BARS, FORGINGS, AND RINGS, 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740) |
| SAE AMS6427M | STEEL BARS, FORGINGS, AND TUBING, 0.88CR - 1.8NI - 0.42MO - 0.08V (0.25 - 0.33C) (4330 MOD) |
| SAE AMS 6547 : 2013 | STEEL BARS, FORGINGS, AND TUBINGS, 1.0CR - 3.2NI - 0.2MO - (0.12 - 0.17C), AIRCRAFT QUALITY |
| SAE AMS6382P | STEEL, BARS, FORGINGS, AND RINGS 0.95CR - 0.20MO (0.38 - 0.43C) (SAE 4140) ANNEALED |
| SAE AMS6432C | STEEL BARS, FORGINGS, AND TUBING, 1.05CR - 0.55NI - 1.0MO - 0.12V (0.43-0.49C) |
| SAE AMS6274R | STEEL BARS, FORGINGS AND TUBING, 0.50CR - 0.55NI - 0.20MO (0.18 - 0.23C) (SAE 8620) |
| SAE AMS6300G | STEEL BARS AND FORGINGS, 0.25MO (0.35 - 0.40C) (SAE 4037) |
| SAE ARP1917A | CLARIFICATION OF TERMS USED IN AEROSPACE METALS SPECIFICATIONS |
| SAE AMS6359K | STEEL, SHEET, STRIP, AND PLATE 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) |
| SAE AMS 6494 : 2016 | STEEL BARS, FORGINGS, AND TUBING, 1.0CR - 2.50NI - 2.0MO - 1.10SI (0.10 - 0.20C) AIRCRAFT-QUALITY |
| SAE AMS6264L | STEEL, CARBURIZING GRADE, BARS, FORGINGS, AND TUBING 1.2CR - 3.2NI - 0.12MO (0.14 - 0.20C) (9317) |
| SAE AMS6290J | STEEL, BARS AND FORGINGS, CARBURIZING, 1.8NI - 0.25MO (0.11 - 0.17C) (SAE 4615) |
| SAE AMS6348D | STEEL, BARS, 0.95CR - 0.20MO (0.28 TO 0.33C) (SAE 4130), NORMALIZED |
| SAE AMS6422K | STEEL, BARS, FORGINGS, AND TUBING, 0.80CR - 0.85NI - 0.20MO - 0.003B - 0.04V (0.38 - 0.43C) (MODIFIED 98BV40) |
| SAE J421_201801 | CLEANLINESS RATING OF STEELS BY THE MAGNETIC PARTICLE METHOD |
| SAE AMS S 6758 : 2017 | STEEL, CHROME-MOLYBDENUM (4130) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) |
| SAE AMS6451D | STEEL, SPRING WIRE, 1.4SI - 0.65CR (0.51 - 0.59C) (SAE 9254) OIL TEMPERED |
| SAE AMS6412N | STEEL, BARS AND FORGINGS 0.80CR - 1.8NI - 0.25MO (0.35 - 0.40C) (4337) |
| BS 6S 100:2010 | Aerospace series. Procedure for inspection, testing and acceptance of wrought steels (other than plate, sheet, strip and tube) |
| SAE AMS6280M | STEEL BARS, FORGINGS, AND RINGS, 0.50CR - 0.55NI - 0.20MO (0.28 - 0.33C) (SAE 8630) |
| SAE AMS6304M | LOW-ALLOY STEEL, HEAT-RESISTANT, BARS, FORGINGS, AND TUBING, 0.95CR - 0.55MO - 0.30V (0.40 - 0.50C) |
| SAE AMS6320P | STEEL BARS, FORGINGS, AND RINGS 0.50CR - 0.55NI - 0.25MO (0.33 - 0.38C) (8735) |
| SAE AMS 6484 : 2016 | STEEL, BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) NORMALIZED AND TEMPERED |
| SAE AMS6455L | STEEL, SHEET, STRIP, AND PLATE, 0.95CR - 0.22V (0.48 - 0.53C) (SAE 6150) |
| MIL-S-81054 Revision A:1976 | STEEL, BARS AND FORGINGS, CHROMIUM NICKEL MOLYBDENUM VANADIUM (FOR TORPEDO MK 46 MOD O) |
| SAE AMS6423H | STEEL BARS, FORGINGS, AND TUBING, 0.92CR - 0.75NI - 0.52MO - 0.003B - 0.04V (MODIFIED 98BV40) |
| SAE AMS6325K | STEEL, BARS, AND FORGINGS 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740) HEAT TREATED, 105 KSI (724 MPA) TENSILE STRENGTH |
| SAE AMS6358K | STEEL SHEET, STRIP, AND PLATE, 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740) |
| SAE AIR4777B | NONDESTRUCTIVE INSPECTION (NDI) METHODS USED DURING PRODUCTION AND OPERATION OF AIRCRAFT WHEELS AND BRAKES |
| SAE AMS6385K | STEEL SHEET, STRIP, AND PLATE, LOW ALLOY, HEAT-RESISTANT, 0.65SI - 1.25CR - 0.50MO - 0.25V (0.27 - 0.33C) |
| SAE AMS 6539 : 2013 | STEEL BARS, FORGINGS, AND TUBING, 1.7CR - 3.8NI - 0.3MO - (0.32-0.38 C), AIRCRAFT-QUALITY |
| SAE AMS6292J | STEEL BARS AND FORGINGS, CARBURIZING 1.8NI - 0.25MO (0.15 - 0.20C) (SAE 4617) |
| SAE AMS6324J | STEEL BARS, FORGINGS, AND TUBING, 0.65CR - 0.70NI - 0.25MO (0.38 - 0.43C) (8740 MODIFIED) |
| SAE AMS6415U | STEEL, BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) |
| SAE AMS6381J | STEEL, MECHANICAL TUBING, 0.95CR - 0.20MO (0.38 - 0.43C) (SAE 4140) |
| SAE AMS6270Q | STEEL, BARS, FORGINGS, AND TUBING 0.50CR - 0.55NI - 0.20MO (0.13 - 0.18C) (SAE 8615) |
| SAE AMS6365K | STEEL TUBING, SEAMLESS, 0.95CR - 0.20MO (0.33 - 0.38C) (SAE 4135), NORMALIZED OR STRESS RELIEVED |
| ASTM E 709 : 2015 : REDLINE | Standard Guide for Magnetic Particle Testing |
| SAE AMS6281J | STEEL, MECHANICAL TUBING, 0.50CR - 0.55NI - 0.20MO (0.28 - 0.33C) (SAE 8630) |
| AGMA 2101 : D | FUNDAMENTAL RATING FACTORS AND CALCULATION METHODS FOR INVOLUTE SPUR AND HELICAL GEAR TEETH (METRIC EDITION) |
| SAE AMS6470N | STEEL, NITRIDING, BARS, FORGINGS, AND TUBING 1.6CR - 0.35MO - 1.13AL (0.38 - 0.43C) (135 MOD) |
| AGMA 2001 : D | FUNDAMENTAL RATING FACTORS AND CALCULATION METHODS FOR INVOLUTE SPUR AND HELICAL GEAR TEETH |
| SAE AMS6374D | STEEL TUBING, SEAM-FREE, ROUND, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), 95.0 KSI (655 MPA) TENSILE STRENGTH |
| SAE AMS S 6098 : 1999 | STEEL, CHROME-NICKEL-MOLYBDENUM (8735) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) |
| SAE AMST5066A | TUBING, CARBON STEEL (1025), (AIRCRAFT QUALITY) |
| MIL S 18728 : D | STEEL PLATE, SHEET, AND STRIP, ALLOY, 8630, AIRCRAFT QUALITY |
| AGMA 923 : B | METALLURGICAL SPECIFICATIONS OF STEEL GEARING |
| SAE AMS6294J | STEEL BARS AND FORGINGS, CARBURIZING 1.8NI - 0.25MO (0.17 - 0.22C) (SAE 4620) |
| SAE AMS6450K | STEEL, SPRING WIRE 0.95CR - 0.22V (0.48 - 0.53C) (SAE 6150) ANNEALED AND COLD DRAWN |
| SAE AMS 6260S : 2016 | STEEL, BARS, FORGINGS, AND TUBING, 1.2CR - 3.2NI - 0.12MO (0.07 - 0.13C) (9310) |
| MIL-S-8503 Revision B:1978 | STEEL BARS, CHROME-VANADIUM (6150) AIRCRAFT QUALITY |
| SAE AMS6430J | STEEL, BARS, FORGINGS, TUBING, AND RINGS, 0.75MN - 0.78CR - 1.8NI - 0.35MO - 0.20V (0.32 - 0.38C), (4335 MODIFIED) |
| MIL-S-18729 Revision C:1965 | STEEL PLATE, SHEET, AND STRIP, ALLOY, 4130, AIRCRAFT QUALITY |
| SAE AMS6372N | STEEL, MECHANICAL TUBING, 0.95CR - 0.20MO (0.33 - 0.38C) (SAE 4135) |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| SAE AMS 6496 : 2013 | STEEL BARS, FORGINGS, AND TUBING, NITRIDING, 1.4CR - 1.2MO - 0.3V (0.29 - 0.36C) AIRCRAFT-QUALITY FOR BEARING APPLICATIONS |
| SAE AMS6362G | STEEL TUBING, SEAMLESS, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), 150 KSI (1034 MPA) TENSILE STRENGTH |
| SAE AMS6272M | STEEL BARS, FORGINGS, AND TUBING 0.50CR - 0.55NI - 0.20MO (0.15 - 0.20C) (SAE 8617) |
| SAE AMS6312J | STEEL BARS, FORGINGS, AND TUBING, 1.8NI - 0.25MO (0.38 - 0.43C) (4640) |
| SAE AMS S 6050 : 1998 | STEEL, CHROME-NICKEL-MOLYBDENUM (8630) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) |
| SAE AMS6323M | STEEL, MECHANICAL TUBING 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740) |
| SAE AMS6250M | STEEL BARS, FORGINGS, AND TUBING, 1.5CR - 3.5NI (0.07 - 0.13C) (3310) |
| SAE AMS6437J | STEEL, SHEET, STRIP, AND PLATE, 5.0CR - 1.3MO - 0.50V (0.38 - 0.43C) (H-11) |
| SAE AMS6373H | STEEL, WELDED TUBING, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130) |
| SAE AMS6448L | STEEL, BARS, FORGINGS AND TUBING 0.95CR - 0.22V (0.48 - 0.53C) (SAE 6150) |
| SAE AMS6346B | STEEL BARS, 0.95CR - 0.20MO (0.28 TO 0.33C) (SAE 4130), HARDENED AND TEMPERED, 125 KSI (862 MPA) TENSILE STRENGTH |
| SAE AMS6424G | STEEL BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.49 - 0.55C) |
| ISO 81400-4:2005 | Wind turbines Part 4: Design and specification of gearboxes |
| SAE AMS6356H | STEEL, SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO - (0.30 - 0.35C) (4132) |
| MIL-I-6868 Revision E:1976 | INSPECTION PROCESS, MAGNETIC PARTICLE |
| SAE AMS6342K | STEEL BARS, FORGINGS, AND TUBING, 0.80CR - 1.0NI - 0.25MO (0.38 - 0.43C) (SAE 9840) |
| SAE AMS6421G | STEEL BARS, FORGINGS, AND TUBING 0.80CR - 0.85NI - 0.20MO - 0.003B (0.35 - 0.40C) (MODIFIED 98B37) |
| MIL-S-8690 Revision B:1978 | STEEL, CHROME NICKEL MOLYBDENUM 8620, BARS AIRCRAFT QUALITY |
| AGMA 2004 : C | GEAR MATERIALS, HEAT TREATMENT AND PROCESSING MANUAL |
| SAE AMS6395H | STEEL SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.38 - 0.43C) (SAE 4140) |
| SAE AMS6413M | STEEL, MECHANICAL TUBING 0.80CR - 1.8NI - 0.25MO (0.35 - 0.40C) (4337) |
| SAE AMS6475K | STEEL, NITRIDING, BARS, FORGINGS, AND TUBING, 1.1CR - 3.5NI - 0.25MO - 1.2AL (0.21 - 0.26C) |
| MIL-T-13915 Revision E:1987 | TUBE, STEEL , SEAMLESS, FOR CANNONS AND RECOILLESS RIFLES |
| 09/30199785 DC : 0 | BS 6S 100 - PROCEDURE FOR INSPECTION, TESTING AND ACCEPTANCE OF WROUGHT STEELS (OTHER THAN PLATE, SHEET, STRIP AND TUBE) |
| SAE MAM6304B | LOW-ALLOY STEEL, HEAT-RESISTANT, BARS, FORGINGS, AND TUBING, 0.95CR - 0.55MO - 0.30V (0.40 - 0.50C) |
| BS ISO 81400-4:2005 | Wind turbines Design and specification of gearboxes |
| SAE AMS6357L | STEEL SHEET, STRIP, AND PLATE, 0.50CR - 0.55NI - 0.25MO (0.33 - 0.38C) (8735) |
| SAE AMS6407K | STEEL, BARS, FORGINGS, AND TUBING, 1.2CR - 2.0NI - 0.45MO (0.27 - 0.33C) |
| SAE AMS6317K | STEEL BARS AND FORGINGS, 1.8NI - 0.25MO (0.38 - 0.43C) (4640), HEAT TREATED, 125 KSI (862 MPA) TENSILE STRENGTH |
| SAE AMS6349E | STEEL BARS, 0.95CR - 0.20MO (0.38 TO 0.43C) (SAE 4140), NORMALIZED |
| SAE AMS7301J | Steel, Highly-Stressed Springs 0.95Cr - 0.20V (0.48 - 0.53C) (SAE 6150) Case Hardened(STABILIZED Aug 2017) |
| SAE AMS6440S | STEEL, BARS, FORGINGS, AND TUBING, 1.45CR (0.93 - 1.05C) (SAE 52100), FOR BEARING APPLICATIONS |
| SAE AMS6330J | STEEL BARS, FORGINGS, AND TUBING, 0.65CR - 1.25NI (0.33 - 0.38C) |
| SAE AMS6371L | STEEL, MECHANICAL TUBING, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130) |
| SAE AMS6345D | STEEL, SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), NORMALIZED OR OTHERWISE HEAT TREATED |
| ASTM A 646/A646M : 2017 : REDLINE | Standard Specification for Premium Quality Alloy Steel Blooms and Billets for Aircraft and Aerospace Forgings |
| SAE AMS 6428 : 2014 | STEEL, BARS, FORGINGS, AND TUBING 0.78CR - 1.8NI - 0.35MO - 0.20V (0.32 - 0.38C) (4335 MOD) |
| SAE AMS6472F | STEEL, BARS AND FORGINGS, NITRIDING 1.6CR - 0.35MO - 1.1AL (0.38 - 0.43C) (135 MOD) HARDENED AND TEMPERED, 112 KSI (772 MPA) TENSILE STRENGTH |
| SAE AMS6475L | Steel, Nitriding, Bars, Forgings, and Tubing 1.1Cr - 3.5Ni - 0.25Mo - 1.2Al (0.21 - 0.26C) |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| ASTM E 10 : 2017-05 | TEST METHOD FOR BRINELL HARDNESS OF METALLIC MATERIALS |
| ASTM E 1444 : 2005 | Standard Practice for Magnetic Particle Testing |
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